Enhanced layerwise model for laminates with imperfect interfaces - Part 2: Experimental validation and failure prediction

被引:1
作者
Mendoza-Navarro, Luis-Ernesto [1 ]
Diaz-Diaz, Alberto [1 ]
Caron, Jean-Francois [2 ]
Chataigner, Sylvain [3 ]
机构
[1] Ctr Invest Mat Avanzados, Ci Chihuahua 31109, Chihuahua, Mexico
[2] Univ Paris Est, Inst Navier, LAMI Ecole Ponts, F-77455 Marne La Vallee, France
[3] LUNAM Univ, IFSTTAR Ctr Nantes, SOA, F-443441 Bouguenais, France
关键词
Interfaces; Adhesive joints; Failure; Plasticity; Layerwise model; ADHESIVE JOINTS; MULTILAYERED MATERIALS; FINITE-ELEMENTS; LIMIT ANALYSIS; DELAMINATION; BEHAVIOR; PLATES; ONSET; STRESSES; STRAIN;
D O I
10.1016/j.compstruct.2011.11.023
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
In this paper, the layerwise model for laminates with imperfect interfaces and enhanced in Part 1 of this work is confronted with experimental results. The model calculations are validated by comparing its sliding predictions in double lap adhesive joints to the sliding measurements performed in a previous paper. The model predictions agree with the experimental results. Finally, the model is applied to the failure analysis in double lap joints and T-peel joints exhibiting adherend, adhesive and cohesive failures. The model calculations and pertinent failure criteria provide accurate predictions and may become a helpful tool suitable to the design of adhesive joints. (C) 2011 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1032 / 1037
页数:6
相关论文
共 36 条
[11]   ANALYZING STRUCTURAL ADHESIVE JOINTS FOR FAILURE [J].
CROCOMBE, AD ;
BIGWOOD, DA ;
RICHARDSON, G .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 1990, 10 (03) :167-178
[12]   Techniques to reduce the peel stresses in adhesive joints with composites [J].
da Silva, Lucas F. M. ;
D Adams, R. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2007, 27 (03) :227-235
[13]   Limit analysis of multi-layered plates. Part II: Shear effects [J].
Dallot, Julien ;
Sab, Karam .
JOURNAL OF THE MECHANICS AND PHYSICS OF SOLIDS, 2008, 56 (02) :581-612
[14]  
Davila C. G., 2003, Technical Report NASA/TM-2003-212663
[15]  
DELOSRIOS GSA, 2009, MODEL SIMUL MATER SC, V17, P1
[16]   Interface plasticity and delamination onset prediction [J].
Diaz, AD ;
Caron, JF .
MECHANICS OF MATERIALS, 2006, 38 (07) :648-663
[17]   Prediction of the onset of mode III delamination in carbon-epoxy laminates [J].
Diaz, AD ;
Caron, JF .
COMPOSITE STRUCTURES, 2006, 72 (04) :438-445
[18]   Analysis of laminated shells by a sinusoidal shear deformation theory and radial basis functions collocation, accounting for through-the-thickness deformations [J].
Ferreira, A. J. M. ;
Carrera, E. ;
Cinefra, M. ;
Roque, C. M. C. ;
Polit, O. .
COMPOSITES PART B-ENGINEERING, 2011, 42 (05) :1276-1284
[19]   High strain-rate compression and tension behaviour of an epoxy bi-component adhesive [J].
Goglio, L. ;
Peroni, L. ;
Peroni, M. ;
Rossetto, M. .
INTERNATIONAL JOURNAL OF ADHESION AND ADHESIVES, 2008, 28 (07) :329-339
[20]   Probabilistic analysis of failure in adhesive bonded joints [J].
Hadj-Ahmed, R ;
Foret, G ;
Ehrlacher, A .
MECHANICS OF MATERIALS, 2001, 33 (02) :77-84